UAS “GRIF-150” is designed for aerial optronic and radiation reconnaissance of the terrain, electronic counteraction to enemy’s radar means, for detection of emergency situations and evaluation of their consequences.
UAS “GRIF-150” includes:
• Unmanned aerial vehicles (2-4 pieces);
• Changeable payload including:
• gyro-stabilized optronic system (GOES) designed to perform imagery reconnaissance in visible and IR spectra;
• airborne radiation monitoring equipment (BARK) designed for operational aerial radiation reconnaissance of the terrain;
• jamming equipment APR and APR-3 designed for jamming receivers of GPS and GLONASS satellite navigation systems, as well as INMARSAT, THURAYA, IRIDIUM satellite communication systems;
• ground-based control post (GBCP) designed for automation of tasks solved by the UAV conducting the mission;
• Ground support means:
• maintenance vehicle (MV) designed to prepare UAV for use, carry out technical maintenance and repair the system;
• transportation vehicle designed for transportation and non-assisted unloading of UAV containers, for searching and carrying back the emergency-landed UAV.
Solved tasks:
• While performing aerial reconnaissance:
• monitoring terrain (water) surface within the assigned area, obtaining television and thermal images of the surface in real-time;
• automated search and detection of ground-based (water-based) objects and definition of coordinates of the selected objects;
• automatic tracking of the ground-based (water-based) objects selected by operator, definition of their speed and heading;
• feeding reconnaissance data in real-time;
• While performing radiation reconnaissance:
• detection of gamma-ray sources;
• While performing radio-electronic counteraction:
• radio-electronic suppression of communication and radar means by jamming.
Peculiarities/advantages:
• Mobility and stand-alone self-sufficiency;
• Capability to be integrated into current or perspective automated control systems for troops and weapons;
• 100% automation of UAV operation starting with preflight control up to UAV landing;
• Capability to control one or two UAVs simultaneously in the air;
• Continuous monitoring of the preset area by replacing the UAV promptly;
• Equipping with modern payloads hardware, communication and data transmission means, ensuring rapid execution of assigned tasks;
• Capability to conduct UAV flight and to operate its onboard equipment beyond direct radio range visibility in automatic mode strictly under the preset program;
• Capability to carry out assigned tasks in visual and instrument weather conditions, in autonomous mode (if airfield network is not available);
• Particularly robust airframes desing of airframes ensuring their multiple application;
• Low operating cost;
• Skilled staff is not required to operate the system.
Production of systems meets International Standards and com¬plies with the ecological and safety requirements.
Guarantee service life of supplied system – 12 months.
Supplier’s quality management system has been certified to meet the requirements of СТБ ISO 9001-2009.
Technical specifications
Quantity of simultaneously controlled UAVs, pcs
|
up to 2
|
UAV’s takeoff, flight and landing
|
in automatic and automated modes
|
Range of flight, km
|
up to 150
|
Height of flight, m
|
up to 3000
|
Duration of UAV flight, hours
|
up to 5
|
Type of navigation system
|
inertial with correction from satellite radio navigation systems
|
Type of payload
|
gyro-stabilized optronic system; radiation control air-borne equipment; jamming equipment
|
Accuracy of coordinates definition, not more than, m
|
50
|
Type of receiver and transmitter equipment
|
RM-B-01
|
Data transfer rate from UAV to GBCP, Mbit/sec
|
5
|
| Data transfer rate from GBCP to UAV, Mbit/sec |
0,1
|
